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NUMERICAL ANALYSIS OF THE TRANSIENT RESPONSE OF ADVANCED THERMAL PROTECTION SYSTEMS FOR ATMOSPHERIC ENTRY.

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BookPublisher: Nasa, Washington, D.C. 1962Description: 39.DDC classification: NASA | TN D-1370

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-1370 (Browse shelf)	Not for loan		TR7466

Total holds: 0

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Previous	NASA TN D-1367 INVESTIGATION OF THE DAMPING OF LIQUIDS IN RIGHT-CIRCULAR CYLINDRICAL TANKS, INCLUDING THE EFFECTS OF A TIME-VARIANT LIQUID DEPTH.	NASA TN D-1368 STUDY OF UMBRELLA-TYPE ERECTABLE PARABOLOIDAL SOLAR CONCENTRATORS FOR GENERATION OF SPACECRAFT AUXILIARY POWER..	NASA TN D-1369 TEMPERATURE CONTROL OF THE EXPLORER IX SATELLITE.	NASA TN D-1370 NUMERICAL ANALYSIS OF THE TRANSIENT RESPONSE OF ADVANCED THERMAL PROTECTION SYSTEMS FOR ATMOSPHERIC ENTRY.	NASA TN D-1377 DESCRIPTION AND PRELIMINARY CALIBRATION TESTS OF A SMALL ARC-HEATED HYPERSONIC WIND TUNNEL	NASA TN D-1378 AERODYNAMIC HEATING AND BOUNDARY-LAYER TRANSITION ON A 1/10-POWER NOSE SHAPE IN FREE FLIGHT AT MACH NUMBERS UP TO 16 MULTIPLE 10 TO THE POWER 6	NASA TN D-1379 STATIC LONGITUDINAL STABILITY AND PERFORMANCE OF SEVERAL BALLISTIC SPACECRAFT CONFIGURATIONS IN HELIUM AT MACH NUMBER OF 24.5	Next

Bounds With Nasa Tn D-1361-69, 1370

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